Garmin G1000 for Cessna CitationJet User guide

G1000

®

Integrated Flight Deck

Pilot’s Guide

Cessna CitationJet

Model 525

Garmin G1000 Pilot’s Guide for the Cessna CitationJet Model 525

This manual reﬂects the operation of System Software version 1162.00 or later for the Cessna CitationJet Model 525. Some differences in

operation may be observed when comparing the information in this manual to earlier or later software versions.

Garmin International, Inc., 1200 East 151st Street, Olathe, Kansas 66062, U.S.A.

Tel: 913/397.8200 Fax: 913/397.8282

Garmin AT, Inc., 2345 Turner Road SE, Salem, OR 97302, U.S.A.

Tel: 503/391.3411 Fax 503/364.2138

Garmin (Europe) Ltd, Liberty House, Bulls Copse Road, Hounsdown Business Park, Southampton, SO40 9RB, U.K.

Tel: 44/0870.8501241 Fax: 44/0870.8501251

Garmin Corporation, No. 68, Jangshu 2nd Road, Shijr, Taipei County, Taiwan

Tel: 886/02.2642.9199 Fax: 886/02.2642.9099

For after-hours emergency, aircraft on ground (AOG) technical support for Garmin panel mount and integrated avionics systems, please

contact Garmin’s AOG Hotline at 913.397.0836.

Web Site Address: www.garmin.com

Except as expressly provided herein, no part of this manual may be reproduced, copied, transmitted, disseminated, downloaded or stored

in any storage medium, for any purpose without the express written permission of Garmin. Garmin hereby grants permission to download

a single copy of this manual and of any revision to this manual onto a hard drive or other electronic storage medium to be viewed for per-

sonal use, provided that such electronic or printed copy of this manual or revision must contain the complete text of this copyright notice

and provided further that any unauthorized commercial distribution of this manual or any revision hereto is strictly prohibited.

Garmin

®

and G1000

®

are registered trademarks of Garmin Ltd. or its subsidiaries. WATCH

®

, FliteCharts

®

, and SafeTaxi

®

are trademarks of

Garmin Ltd. or its subsidiaries. These trademarks may not be used without the express permission of Garmin.

Bendix/King

®

and Honeywell

®

are registered trademarks of Honeywell International, Inc.; Becker

®

is a registered trademark of Becker

Flugfunkwerk GmbH; NavData

®

is a registered trademark of Jeppesen, Inc.; XM

®

is a registered trademark of XM Satellite Radio, Inc.

May, 2010 190-01131-00 Rev. A Printed in the U.S.A.

Garmin G1000 Pilot’s Guide for the Cessna CitationJet Model 525

LIMITED WARRANTY

190-01131-00 Rev. A

LIMITED WARRANTY

This Garmin product is warranted to be free from defects in materials or workmanship for two years from the date of purchase. Within this

period, Garmin will, at its sole option, repair or replace any components that fail in normal use. Such repairs or replacement will be made

at no charge to the customer for parts and labor, provided that the customer shall be responsible for any transportation cost. This warranty

does not cover failures due to abuse, misuse, accident, or unauthorized alterations or repairs.

THE WARRANTIES AND REMEDIES CONTAINED HEREIN ARE EXCLUSIVE AND IN LIEU OF ALL OTHER WARRANTIES EXPRESS OR IMPLIED

OR STATUTORY, INCLUDING ANY LIABILITY ARISING UNDER ANY WARRANTY OF MERCHANTABILITY OR FITNESS FOR A PARTICULAR

PURPOSE, STATUTORY OR OTHERWISE. THIS WARRANTY GIVES YOU SPECIFIC LEGAL RIGHTS, WHICH MAY VARY FROM STATE TO

STATE.

IN NO EVENT SHALL GARMIN BE LIABLE FOR ANY INCIDENTAL, SPECIAL, INDIRECT OR CONSEQUENTIAL DAMAGES, WHETHER

RESULTING FROM THE USE, MISUSE, OR INABILITY TO USE THIS PRODUCT OR FROM DEFECTS IN THE PRODUCT. Some states do not

allow the exclusion of incidental or consequential damages, so the above limitations may not apply to you.

Garmin retains the exclusive right to repair or replace the unit or software, or to offer a full refund of the purchase price, at its sole

discretion. SUCH REMEDY SHALL BE YOUR SOLE AND EXCLUSIVE REMEDY FOR ANY BREACH OF WARRANTY.

To obtain warranty service, contact your local Garmin Authorized Service Center. For assistance in locating a Service Center near you, visit

the Garmin Web site at “http://www.garmin.com” or contact Garmin Customer Service at 800-800-1020.

Garmin G1000 Pilot’s Guide for the Cessna CitationJet Model 525

i

WARNINGS, CAUTIONS, AND NOTES

190-01131-00 Rev. A

WARNING: Navigation and terrain separation must NOT be predicated upon the use of the terrain avoidance

feature. The terrain avoidance feature is NOT intended to be used as a primary reference for terrain avoidance

and does not relieve the pilot from the responsibility of being aware of surroundings during ﬂight. The

terrain avoidance feature is only to be used as an aid for terrain avoidance. Terrain data is obtained from

third party sources. Garmin is not able to independently verify the accuracy of the terrain data.

WARNING: The displayed minimum safe altitudes (MSAs) are only advisory in nature and should not be

relied upon as the sole source of obstacle and terrain avoidance information. Always refer to current

aeronautical charts for appropriate minimum clearance altitudes.

WARNING: The altitude calculated by the GPS receivers is geometric height above Mean Sea Level and

could vary signiﬁcantly from the altitude displayed by pressure altimeters, such as the GDC 74B Air Data

Computer, or other altimeters in aircraft. GPS altitude should never be used for vertical navigation. Always

use pressure altitude displayed by the PFD or other pressure altimeters in aircraft.

WARNING: Do not use outdated database information. Databases used in the system must be updated

regularly in order to ensure that the information remains current. Pilots using any outdated database do so

entirely at their own risk.

WARNING: Do not use basemap (land and water data) information for primary navigation. Basemap data is

intended only to supplement other approved navigation data sources and should be considered as an aid to

enhance situational awareness.

WARNING: Trafﬁc information shown on system displays is provided as an aid in visually acquiring trafﬁc.

Pilots must maneuver the aircraft based upon TCAS II Resolution Advisories (if installed), ATC guidance, or

positive visual acquisition of conﬂicting trafﬁc.

WARNING: XM Weather should not be used for hazardous weather penetration. Weather information

provided by the GDL 69 is approved only for weather avoidance, not penetration.

WARNING: NEXRAD weather data is to be used for long-range planning purposes only. Due to inherent

delays in data transmission and the relative age of the data, NEXRAD weather data should not be used for

short-range weather avoidance.

WARNING: The Garmin G1000, as installed in the Cessna CitationJet Model 525 aircraft, has a very high

degree of functional integrity. However, the pilot must recognize that providing monitoring and/or self-

test capability for all conceivable system failures is not practical. Although unlikely, it may be possible for

erroneous operation to occur without a fault indication shown by the system. It is thus the responsibility

of the pilot to detect such an occurrence by means of cross-checking with all redundant or correlated

information available in the cockpit.

WARNING: For safety reasons, system operational procedures must be learned on the ground.

Garmin G1000 Pilot’s Guide for the Cessna CitationJet Model 525

ii

WARNINGS, CAUTIONS, AND NOTES

190-01131-00 Rev. A

WARNING: The United States government operates the Global Positioning System and is solely responsible

for its accuracy and maintenance. The GPS system is subject to changes which could affect the accuracy and

performance of all GPS equipment. Portions of the system utilize GPS as a precision electronic NAVigation

AID (NAVAID). Therefore, as with all NAVAIDs, information presented by the system can be misused or

misinterpreted and, therefore, become unsafe.

WARNING: To reduce the risk of unsafe operation, carefully review and understand all aspects of the G1000

Pilot’s Guide documentation and the Cessna CitationJet Model 525 Airplane Flight Manual. Thoroughly

practice basic operation prior to actual use. During ﬂight operations, carefully compare indications from the

system to all available navigation sources, including the information from other NAVAIDs, visual sightings,

charts, etc. For safety purposes, always resolve any discrepancies before continuing navigation.

WARNING: The illustrations in this guide are only examples. Never use the system to attempt to penetrate

a thunderstorm. Both the FAA Advisory Circular, Subject: Thunderstorms, and the

Aeronautical

Information

Manual (AIM) recommend avoiding “by at least 20 miles any thunderstorm identiﬁed as severe or giving an

intense radar echo.”

WARNING:

Lamp(s) inside this product may contain mercury (HG) and must be recycled or disposed of

according to local, state, or federal laws. For more information, refer to our website at www.garmin.com/

aboutGarmin/environment/disposal.jsp.

WARNING:

Because of variation in the earth’s magnetic ﬁeld, operating the system within the following

areas could result in loss of reliable attitude and heading indications. North of 72° North latitude at all

longitudes. South of 70° South latitude at all longitudes. North of 65° North latitude between longitude

75° W and 120° W. (Northern Canada). North of 70° North latitude between longitude 70° W and 128° W.

(Northern Canada). North of 70° North latitude between longitude 85° E and 114° E. (Northern Russia).

South of 55° South latitude between longitude 120° E and 165° E. (Region south of Australia and New

Zealand).

WARNING:

Do not use GPS to navigate to any active waypoint identiﬁed as a ‘NON WGS84 WPT’ by a

system message. ‘NON WGS84 WPT’ waypoints are derived from an unknown map reference datum that

may be incompatible with the map reference datum used by GPS (known as WGS84) and may be positioned

in error as displayed.

CAUTION: The PFD and MFD displays use a lens coated with a special anti-reﬂective coating that is very

sensitive to skin oils, waxes, and abrasive cleaners. CLEANERS CONTAINING AMMONIA WILL HARM THE

ANTI-REFLECTIVE COATING. It is very important to clean the lens using a clean, lint-free cloth and an

eyeglass lens cleaner that is speciﬁed as safe for anti-reﬂective coatings.

CAUTION: The system does not contain any user-serviceable parts. Repairs should only be made by an

authorized Garmin service center. Unauthorized repairs or modiﬁcations could void both the warranty and

the pilot’s authority to operate this device under FAA/FCC regulations.

Garmin G1000 Pilot’s Guide for the Cessna CitationJet Model 525

iii

WARNINGS, CAUTIONS, AND NOTES

190-01131-00 Rev. A

NOTE: All visual depictions contained within this document, including screen images of the panel and

displays, are subject to change and may not reﬂect the most current system and databases. Depictions of

equipment may differ slightly from the actual equipment.

NOTE: This device complies with part 15 of the FCC Rules. Operation is subject to the following two conditions:

(1) this device may not cause harmful interference, and (2) this device must accept any interference received,

including interference that may cause undesired operation.

NOTE: This product, its packaging, and its components contain chemicals known to the State of California

to cause cancer, birth defects, or reproductive harm. This notice is being provided in accordance with

California’s Proposition 65. If you have any questions or would like additional information, please refer to

our web site at www.garmin.com/prop65.

NOTE

: Interference from GPS repeaters operating inside nearby hangars can cause an intermittent loss of

attitude and heading displays while the aircraft is on the ground. Moving the aircraft more than 100 yards

away from the source of the interference should alleviate the condition.

NOTE

: Use of polarized eyewear may cause the ﬂight displays to appear dim or blank.

Garmin G1000 Pilot’s Guide for the Cessna CitationJet Model 525

iv

WARNINGS, CAUTIONS, AND NOTES

190-01131-00 Rev. A

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Garmin G1000 Pilot’s Guide for the Cessna CitationJet Model 525

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REVISION INFORMATION

190-01131-00 Rev. A

Record of Revisions

Part Number Revision Date Page Range Description

190-01131-00 A May, 2010 All Initial release

Garmin G1000 Pilot’s Guide for the Cessna CitationJet Model 525

vi

REVISION INFORMATION

190-01131-00 Rev. A

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Garmin G1000 Pilot’s Guide for the Cessna CitationJet Model 525

vii

TABLE OF CONTENTS

190-01131-00 Rev. A

SECTION 1 SYSTEM OVERVIEW

1.1 System Description ................................................. 1

1.2 Line Replaceable Units (LRU) ................................. 2

1.3 G1000 Controls ........................................................ 8

PFD Controls ................................................................ 8

MFD Control Unit ....................................................... 10

AFCS Controls ............................................................ 11

Audio Panel Controls .................................................. 13

1.4 Secure Digital Cards.............................................. 15

1.5 System Power-up ................................................... 16

1.6 System Operation .................................................. 17

Normal Operation ....................................................... 17

Reversionary Mode ..................................................... 17

AHRS Operation ......................................................... 19

G1000 System Annunciations ...................................... 20

Softkey Function ......................................................... 21

GPS Receiver Operation .............................................. 28

1.7 Accessing G1000 Functionality............................ 33

Menus ....................................................................... 33

MFD Page Groups ....................................................... 33

MFD System Pages...................................................... 37

1.8 Display Backlighting ............................................. 46

Automatic Adjustment ................................................ 46

Manual Adjustment .................................................... 46

SECTION 2 FLIGHT INSTRUMENTS

2.1 Flight Instruments .................................................52

Airspeed Indicator ...................................................... 52

Attitude Indicator ....................................................... 55

Altimeter ................................................................... 57

Vertical Speed Indicator (VSI) ....................................... 61

Vertical Deviation ....................................................... 61

Horizontal Situation Indicator (HSI) .............................. 62

Course Deviation Indicator (CDI) .................................. 67

2.2 Supplemental Flight Data .................................... 75

Temperature Displays .................................................. 75

Wind Data ................................................................. 76

Vertical Navigation (VNV) Indications ........................... 77

2.3 PFD Annunciations and Alerting Functions ........ 78

System Alerting .......................................................... 78

Marker Beacon Annunciations...................................... 79

Trafﬁc Annunciations................................................... 79

TAWS Annunciations ................................................... 80

Minimum Descent Altitude/Decision Height Alerting ......80

Altitude Alerting ......................................................... 82

Low Altitude Annunciation .......................................... 82

Radar Altimeter .......................................................... 83

2.4 Abnormal Operations ........................................... 85

Abnormal GPS Conditions ........................................... 85

Unusual Attitudes ....................................................... 86

SECTION 3 ENGINE INDICATION SYSTEM (EIS)

3.1 Engine Indication System (EIS) ............................ 90

Ground OAT Set Window ............................................. 91

Engine Spool Rotation Speeds (N1 and N2) ................... 92

Oil Pressure and Temperature ...................................... 94

Fuel Display ............................................................... 94

Inter-Turbine Temperature ............................................ 95

SECTION 4 AUDIO PANEL AND CNS

4.1 Overview ................................................................ 97

Audio Panel Volume Control ........................................ 97

PFD Controls and Frequency Display ............................. 98

Audio Panel Controls ................................................ 100

4.2 COM Operation .................................................... 102

COM Transceiver Selection and Activation ................... 102

COM Transceiver Manual Tuning ................................ 103

Quick-tuning and Activating 121.500 MHz .................. 104

Auto-tuning the COM Frequency ................................ 105

Frequency Spacing .................................................... 109

Automatic Squelch .................................................... 110

Volume .................................................................... 110

4.3 NAV Operation ..................................................... 111

NAV Radio Selection and Activation ........................... 111

NAV Receiver Manual Tuning ..................................... 112

Auto-tuning a NAV Frequency from the MFD ............... 114

Marker Beacon Receiver ............................................ 118

DME Tuning ............................................................. 119

4.4 Mode S Transponder ........................................... 120

GTX 33/33D Transponder Controls .............................. 120

GTX 33/33D Transponder Mode Selection.................... 121

Entering a Transponder Code ..................................... 123

IDENT Function ........................................................ 124

Flight ID Reporting.................................................... 125

Garmin G1000 Pilot’s Guide for the Cessna CitationJet Model 525

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TABLE OF CONTENTS

190-01131-00 Rev. A

4.5 Additional Audio Panel Functions ..................... 126

Power-up ................................................................. 126

Mono/Stereo Headsets .............................................. 126

Speaker ................................................................... 126

Unmuted Inputs ....................................................... 126

Intercom .................................................................. 127

Passenger Address (PA) System .................................. 128

Simultaneous COM Operation .................................... 128

Clearance Recorder and Player ................................... 129

4.6 Audio Panels Preﬂight Procedure ...................... 130

4.7 Abnormal Operation ........................................... 132

Stuck Microphone ..................................................... 132

COM Tuning Failure ................................................... 132

PFD Failure, Dual System ........................................... 132

Audio Panel Fail-safe Operation ................................. 133

Reversionary Mode ................................................... 133

SECTION 5 FLIGHT MANAGEMENT

5.1 Introduction ......................................................... 135

Navigation Status Box ............................................... 136

5.2 Using Map Displays ............................................. 138

Map Orientation ....................................................... 138

Map Range .............................................................. 140

Map Panning ............................................................ 142

Measuring Bearing and Distance ................................ 146

Topography .............................................................. 147

Map Symbols ........................................................... 150

Airways ................................................................... 156

Track Vector ............................................................. 158

Wind Vector ............................................................. 159

Nav Range Ring........................................................ 160

Fuel Range Ring ....................................................... 161

Field of View (SVS) .................................................... 162

5.3 Waypoints ............................................................. 163

Airports ................................................................... 164

Intersections ............................................................ 171

NDBs ....................................................................... 173

VORs ....................................................................... 175

User Waypoints ........................................................ 177

5.4 Airspaces .............................................................. 183

5.5 Direct-to-Navigation .......................................... 187

5.6 Flight Planning ..................................................... 192

Flight Plan Creation .................................................. 193

Adding Waypoints to an Existing Flight Plan ................ 198

Adding Airways to a Flight Plan ................................. 200

Adding Procedures to a Stored Flight Plan .................. 202

Flight Plan Storage ................................................... 209

Flight Plan Editing .................................................... 211

Along Track Offsets ................................................... 214

Parallel Track ............................................................ 216

Activating a Flight Plan Leg ....................................... 219

Inverting a Flight Plan ............................................... 220

Flight Plan Views ...................................................... 221

Closest Point of FPL .................................................. 223

5.7 Vertical Navigation ............................................. 224

Altitude Constraints .................................................. 226

5.8 Procedures ........................................................... 229

Departures ............................................................... 229

Arrivals ................................................................... 232

Approaches ............................................................. 234

5.9 Trip Planning ........................................................ 240

Trip Planning ............................................................ 240

Weight Planning ....................................................... 244

Weight Caution And Warning Conditions .................... 246

5.10 RAIM Prediction................................................... 247

5.11 Navigating a Flight Plan ..................................... 250

5.12 Abnormal Operation ........................................... 278

SECTION 6 HAZARD AVOIDANCE

6.1 XM Satellite Weather .......................................... 281

Activating Services .................................................... 281

Using XM Satellite Weather Products .......................... 283

6.2 WX-500 Stormscope ........................................... 310

Setting Up Stormscope on the Navigation Map ........... 310

Selecting the Stormscope Page .................................. 314

6.3 Airborne Color Weather Radar .......................... 315

System Description ................................................... 315

Principles of Pulsed Airborne Weather Radar ............... 315

Safe Operating Distance ............................................ 319

Basic Antenna Tilt Setup ............................................ 320

Weather Mapping and Interpretation ......................... 322

Ground Mapping and Interpretation ........................... 335

6.4 TAWS-B ................................................................. 336

Displaying TAWS-B Data ............................................ 337

TAWS-B Page ........................................................... 339

TAWS-B Alerts .......................................................... 341

System Status ........................................................... 347

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TABLE OF CONTENTS

190-01131-00 Rev. A

6.5 TAWS-A ................................................................. 349

TAWS-A Page ........................................................... 351

TAWS-A Alerts .......................................................... 353

System Status ........................................................... 365

TAWS-A Abnormal operations .................................... 366

6.6 Trafﬁc Information Service (TIS) ........................ 369

Displaying TRAFFIC Data ........................................... 370

Trafﬁc Map Page ....................................................... 372

TIS Alerts ................................................................. 373

System Status ........................................................... 375

6.7 Garmin GTS Trafﬁc ............................................... 378

Theory of operation .................................................. 378

TAS Alerts ................................................................ 381

System Test .............................................................. 382

Operation ................................................................ 383

6.8 Honeywell KTA870 Trafﬁc ................................... 392

TAS Symbology ......................................................... 392

Operation ................................................................ 393

Altitude Display ........................................................ 396

Trafﬁc Map Page Display Range ................................. 396

TAS Alerts ................................................................ 398

System Status ........................................................... 399

6.9 L-3 Skywatch Trafﬁc ............................................ 400

TAS Symbology ......................................................... 400

Operation ................................................................ 401

Altitude Display ........................................................ 404

Trafﬁc Map Page Display Range ................................. 404

TAS Alerts ................................................................ 406

System Status ........................................................... 406

SECTION 7 AUTOMATIC FLIGHT CONTROL SYSTEM

7.1 AFCS Controls ...................................................... 410

7.2 Flight Director Operation ................................... 412

Activating the Flight Director ..................................... 412

AFCS Status Box ....................................................... 413

Flight Director Modes ................................................ 414

Switching Flight Directors .......................................... 414

Command Bars ......................................................... 415

7.3 Vertical Modes ..................................................... 416

Pitch Hold Mode (PIT) ............................................... 417

Selected Altitude Capture Mode (ALTS) ....................... 418

Altitude Hold Mode (ALT) .......................................... 419

Vertical Speed Mode (VS) .......................................... 420

Flight Level Change Mode (FLC) ................................. 421

Vertical Navigation Modes (VPTH, ALTV) ..................... 424

Glidepath Mode (GP) ................................................ 429

Glideslope Mode (GS) ............................................... 431

Takeoff (TO) and Go Around (GA) Modes .................... 432

7.4 Lateral Modes ...................................................... 433

Roll Hold Mode (ROL) ............................................... 434

Low Bank Mode ....................................................... 434

Navigation Modes (GPS, VOR, LOC) ............................ 436

Approach Modes (GPS, VAPP, LOC) ............................. 438

Backcourse Mode (BC) .............................................. 439

7.5 Autopilot and Yaw Damper Operation ............. 441

Flight Control ........................................................... 441

Engagement ............................................................. 442

Control Wheel Steering ............................................. 442

Disengagement ........................................................ 443

7.6 Example Flight Plan ............................................ 444

Departure ................................................................ 445

Intercepting a VOR Radial .......................................... 447

Flying a Flight Plan/GPS Course ................................. 448

Descent ................................................................... 449

Approach ................................................................. 452

Go Around/Missed Approach ..................................... 455

7.7 AFCS Annunciations and Alerts .........................457

AFCS Status Alerts .................................................... 457

Overspeed Protection ................................................ 458

SECTION 8 ADDITIONAL FEATURES

8.1 Synthetic Vision System (SVS) ........................... 460

SVS Operation .......................................................... 461

SVS Features ............................................................ 463

Field of View ............................................................ 472

8.2 SafeTaxi ................................................................ 474

8.3 ChartView ............................................................. 480

ChartView Softkeys ................................................... 480

Terminal Procedures Charts ....................................... 481

Chart Options ........................................................... 489

Day/Night View ........................................................ 495

ChartView Cycle Number and Expiration Date ............. 497

8.4 FliteCharts ............................................................ 500

FliteCharts Softkeys .................................................. 500

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TABLE OF CONTENTS

190-01131-00 Rev. A

Terminal Procedures Charts ....................................... 501

Chart Options ........................................................... 508

Day/Night View ........................................................ 512

FliteCharts Cycle Number and Expiration Date ............. 514

8.5 AOPA Airport Directory ....................................... 517

AOPA Database Cycle Number and Revision ............... 518

8.6 Satellite Telephone Services .............................. 520

Registering the Iridium Satellite System ...................... 520

Telephone Communication ........................................ 520

8.7 XM Radio Entertainment .................................... 534

Activating XM Satellite Radio Services ........................ 534

Using XM Radio ....................................................... 536

8.8 Scheduler .............................................................. 539

8.9 Abnormal Operation ........................................... 541

SVS Troubleshooting ................................................. 541

Reversionary Mode ................................................... 541

Unusual Attitudes ..................................................... 542

APPENDICES

Annunciations and Alerts ............................................. 545

Comparator Annunciations ........................................ 547

Reversionary Sensor Annunciations ............................ 547

advisory AnnuNciations ............................................. 548

Message Advisory Alerts ............................................ 548

G1000 System Annunciations .................................... 548

G1000 System Message Advisories ............................. 551

AFCS Alerts .............................................................. 563

TAWS-B ALERTS ........................................................ 564

TAWS-A Alerts (Optional) .......................................... 565

TCAS I Alerts and Annunciations (Optional) ................. 567

Other G1000 Aural Alerts .......................................... 567

Flight Plan Import/Export Messages ........................... 568

Database Management ................................................ 569

Garmin Databases .................................................... 569

Jeppesen Databases .................................................. 570

Automatic Database Synchronization ......................... 571

Loading Updated Databases ...................................... 572

Glossary .......................................................................... 575

Frequently Asked Questions ........................................ 581

General TIS Information ............................................... 585

Introduction ............................................................. 585

TIS vs. TAS/TCAS ....................................................... 585

TIS Limitations.......................................................... 585

Display Symbols ............................................................ 587

INDEX

Index ................................................................................I-1

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Garmin G1000 Pilot’s Guide for the Cessna CitationJet Model 525

1

SYSTEM OVERVIEW

SECTION 1 SYSTEM OVERVIEW

1.1 SYSTEM DESCRIPTION

This section provides an overview of the G1000 Integrated Flight Deck as installed in the Cessna CitationJet

Model 525. The G1000 system is an integrated ﬂight control system that presents ﬂight instrumentation, position,

navigation, communication, and identiﬁcation information to the pilot through large-format displays. The system

consists of the following Line Replaceable Units (LRUs):

•

GDU 1040A

Primary Flight Display (PFD)

•

GDU 1240A

Multi Function Display (MFD)

•

GIA 63W

Integrated Avionics Unit

•

GDC 74B

Air Data Computer (ADC)

•

GEA 71

Engine/Airframe Unit

•

GRS 77

Attitude and Heading Reference System

(AHRS)

•

GMU 44

Magnetometer

•

GMA 1347D-20

Dual Audio System with

Integrated Marker Beacon Receiver

•

GTX 33/33D

Mode S Transponder)

•

GDL 69A

Satellite Data Link Receiver

•

GDL 59

Data Link

•

GSR 56

Iridium Transceiver

•

GWX 68

Weather Radar

•

GCU 475

MFD Control Unit

•

GMC 710

AFCS Control Unit

•

GTS 820/850

Trafﬁc Avoidance System (optional)

•

GA 58

Directional Antenna

•

GTP 59

Outside Air Temperature (OAT) Probe

•

GA 36

GPS/WAAS and

GA 37

GPS/WAAS/XM

Antennas

•

GSA 80

and

GSA 81

AFCS Servos

•

GSM 86

Servo Gearboxes

A top-level G1000 system block diagram is shown in Figure 1-1 (it does not include the GA 36, GA 37, or GSM

86).

NOTE: Refer to the AFCS section for details on the GFC 700 AFCS.

In the Cessna CitationJet Model 525, the GFC 700 Automated Flight Control System (AFCS) provides the ﬂight

director (FD), autopilot (AP), and yaw damper (YD) functions of the G1000 system.

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Garmin G1000 Pilot’s Guide for the Cessna CitationJet Model 525

2

SYSTEM OVERVIEW

1.2 LINE REPLACEABLE UNITS (LRU)

•

GDU 1040A

(2) – Each unit is conﬁgured as a PFD that features a 10.4-inch LCD with 1024 x 768 resolution.

The unit installed on the left/pilot side is designated as PFD1, and the one installed on the right/copilot side

is designated as PFD2. These units communicate with each other, the MFD, and with the on-side GIA 63W

Integrated Avionics Unit through a High-Speed Data Bus (HSDB) connection.

•

GDU 1240A

(1) – Features a 12-inch LCD with 1024 x 768 resolution and is conﬁgured as an MFD. This unit

is linked to both PFDs via HSDB connection.

•

GIA 63W

(2) – Functions as the main communication hub, linking all LRUs with the on-side PFD. Each

GIA 63W contains a GPS WAAS receiver, VHF COM/NAV/GS receivers, a ﬂight director (FD) and system

integration microprocessors. Each GIA 63W is paired with the on-side PFD via HSDB connection. The GIA

63Ws are not paired together and do not communicate with each other directly.

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3

SYSTEM OVERVIEW

•

GDC 74B

(2) – Processes data from the pitot/static system as well as the OAT probe. This unit provides

pressure altitude, airspeed, vertical speed and OAT information to the G1000 system, and it communicates

with the on-side GIA 63W, on-side GDU 1040A and on-side GRS 77, using an ARINC 429 digital interface

(it also interfaces directly with the on-side GTP 59). The GDC 74B is designed to operate in Reduced Vertical

Separation Minimum (RVSM) airspace.

•

GEA 71

(2) – Receives and processes signals from the engine and airframe sensors. This unit communicates

with both GIA 63Ws using an RS-485 digital interface.

•

GRS 77

(2) – Provides aircraft attitude and heading information via ARINC 429 to both the on-side GDU

1040A and the on-side GIA 63W. The GRS 77 contains advanced sensors (including accelerometers and rate

sensors) and interfaces with the on-side GMU 44 to obtain magnetic ﬁeld information, with the GDC 74B to

obtain air data, and with both GIA 63Ws to obtain GPS information. AHRS modes of operation are discussed

later in this document.

•

GMU 44

(2) – Measures local magnetic ﬁeld. Data is sent to the GRS 77 for processing to determine aircraft

magnetic heading. This unit receives power directly from the GRS 77 and communicates with the GRS 77,

using an RS-485 digital interface.

190-01131-00 Rev. A

Garmin G1000 Pilot’s Guide for the Cessna CitationJet Model 525

4

SYSTEM OVERVIEW

•

GMA 1347D-20

(2) – Integrates NAV/COM digital audio, intercom system and marker beacon controls, and

is installed in dual conﬁguration on the outboard side of PFD1 and PFD2. This unit also enables the manual

control of the display reversionary mode (red

DISPLAY BACKUP

button) and communicates with the on-side

GIA 63W, using an RS-232 digital interface.

•

GTX 33

(1)

and GTX 33D

(1 or 2) – Solid-state transponders that provide Modes A, C and S capability.

Transponder #1 (XPDR1) is a GTX 33D, which includes Mode S with diversity. Either the GTX 33 or GTX 33D

may be installed as Transponder #2 (XPDR2). Both transponders can be controlled from either PFD, and only

one transponder can be active at a time. Each transponder communicates with the on-side GIA 63W through

an RS-232 digital interface.

•

GDL 69A

(1) – A satellite radio receiver that provides real-time weather information to the G1000 MFD (and,

indirectly, to the inset map of the PFD) as well as digital audio entertainment. The GDL 69A communicates

with the MFD via HSDB connection. A subscription to the XM Satellite Radio service is required to enable the

GDL 69A capability.

•

GDL 59

(1) – GDL 59 operation is performed with the MFD through the HSDB. Connectivity with the GSR 56

for the Iridium telephone feature is through the RS-232 bus.

190-01131-00 Rev. A

Garmin G1000 Pilot’s Guide for the Cessna CitationJet Model 525

5

SYSTEM OVERVIEW

•

GSR 56

(1) – The Iridium Transceiver operation for voice communication is by means of a telephone handset in

the cabin and pilot and copilot headsets in the cockpit. The tranceiver can also send and receive data provided

by the GDL 59 through the RS-232 bus.

•

GWX 68

(1) – Provides airborne weather and ground mapped radar data to the MFD, via HSDB connection.

•

GCU 475

(1) – Provides the Flight Management System (FMS) controls for the MFD through an RS-232 digital

interface.

•

GMC 710

(1) – Provides the controls for the GFC 700 AFCS through an RS-232 digital interface allowing

communication with both PFDs.

•

GTP 59

(2) – Provides Outside Air Temperature (OAT) data to the on-side GDC 74B.

•

GSA 80

(3),

GSA 81

(1), and

GSM 86

(4) – The GSA 80 servos are used for the automatic control of pitch, roll

and yaw, while the GSA 81 servos are used for the automatic control of pitch trim. These units interface with

each GIA 63W.

The GSM 86 servo gearbox is responsible for transferring the output torque of the GSA 80/81 servo actuator to

the mechanical ﬂight-control surface linkage.

190-01131-00 Rev. A

Garmin G1000 Pilot’s Guide for the Cessna CitationJet Model 525

6

SYSTEM OVERVIEW

•

GTS 820/850

– The GTS 820 Trafﬁc Advisory System (TAS) and GTS 850 TCAS I use active interrogations of

Mode S and Mode C transponders to provide Trafﬁc Advisories to the pilot independent of the air trafﬁc control

system.

•

GA 58

– The GA 58 is directional antenna for the Trafﬁc Avoidance System. One top-mounted directional

antenna is required. Optional bottom mounted antenna offers better threat visibility.

•

GA 36

(1) and

GA 37

(1) – The GA 36 is a through-mount GPS/WAAS antenna. The GA 37 is a through-mount

GPS/WAAS antenna with XM/Data Link.

GA 36 GA 37

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